Enthalpy Exchanger Element, Enthalpy Exchanger Comprising Such Elements And Method For Their Production

ABSTRACT

The present invention provides enthalpy exchanger elements (E, E′, PR, PF) and enthalpy exchangers comprising such elements. Furthermore, the invention discloses a method for producing such enthalpy exchanger elements and enthalpy exchangers, comprising the steps of a) providing an air-permeable sheet element ( 1 ); b) laminating at least one side ( 1   a,    1   b ) of the sheet element ( 1 ) with a thin polymer film ( 3, 4 ) with water vapor transmission characteristics; and c) forming the laminated sheet element ( 1 ) into a desired shape exhibiting a three-dimensional corrugation pattern ( 5, 5 , . . . ).

The present invention refers to enthalpy exchanger elements and enthalpyexchangers comprising such elements. Furthermore, the inventiondiscloses a method for producing such enthalpy exchanger elements andenthalpy exchangers.

It is well known to use different kinds of heat exchangers for differentpurposes. Usually, heat exchangers are used to recover heat energy fromone fluid or medium into another one. This kind of heat energy is calledsensible energy. The heat energy or sensible energy of one fluid,normally air, is recovered into another one which is running adjacent,e.g. parallel, counter or cross flow, to the first where the fluid is atlower temperature. By inversing fluid flows, the exchange between thetwo will generate a cooler fluid. Heat exchangers used for sensibleenergy recovery are usually made of metal or polymer elements. There aredifferent types, as there can be cross flow, parallel flow or counterflow configurations. The elements are defining flow channels betweenthemselves so that the fluids can flow between the elements. Suchdevices are e.g. used in residential and commercial ventilation (HRV).

Another type of energy exchangers refers to the so called latent energywhich includes the moisture in the air. To exchange the latent energy itis known to use desiccant coated metal or polymer substrates ormembranes made from desiccant impregnated cellulose or polymer. Betweenplates made from cellulose or polymer, air passages are defined orcreated to allow the fluids to pass along the surface of the plates,thereby transferring moisture from one fluid to the other one. As themembranes usually have no structural strength, it is known to combinethe membranes with frames or grids which thereby define spacings betweenthe membranes.

In case of a combination of the above, i.e. heat exchange and moistureexchange, the energy exchangers are called enthalpy exchanger. Thoseenthalpy exchangers allow for the exchange of sensible and latentenergy, resulting in total energy recovery.

Membrane materials as currently available are delivered by the roll. Themembrane material is the most critical part of an enthalpy exchanger.The membrane must be fixed and sealed to a kind of grid or frame andarranged in a way to allow for a fluid to flow between each membranelayer. So, it is obvious that enthalpy exchangers of the known art are acompromise. They will usually lose in sensible energy exchange to gainin latent energy exchange as a result of the selective scope andcharacteristics of currently used membranes.

Such an enthalpy exchanger built from respective elements is e.g. WO02/072242 A1. On grids, respective membranes made of fibers arepositioned. Grids containing a membrane or spacers between adjacentmembranes, i.e. spacers and membranes in alternating sequence, arestapled or stacked, thereby altering the direction of the plates inorder to create different air flow directions.

In view of the mentioned state of the art, it is an object of theinvention to provide enthalpy exchanger elements and enthalpy exchangersas well as a method for their production which allow for the creation ofenthalpy exchangers where the efficiency of both sensible energyexchange and latent energy exchange in each enthalpy exchanger elementis increased and where the manufacturing cost of enthalpy exchangerelements and enthalpy exchangers made of such elements is reduced.

It is another object of the invention to provide enthalpy exchangerelements and enthalpy exchangers with a high specific exchange area forwater vapor, as well as a method for their production.

In order to achieve this object, the invention provides a method forproducing enthalpy exchanger elements comprising the steps of

a) providing an air-permeable sheet element;b) laminating at least one side of the sheet element with a thin polymerfilm with water vapor transmission characteristics; andc) forming the laminated sheet element into a desired shape exhibiting athree-dimensional corrugation pattern.

As a result, an enthalpy exchanger element is obtained which allows boththe transfer of heat and water molecules in the form of vapor across theelement from one side of the element to the other side of the elementalmost throughout the entire surface area of the element which now has ahigher specific exchange area than such elements in the prior art. Incontrast, molecules larger or less polar than water molecules, such ascarbon dioxide and odor-related molecules, are barred from passingacross the element. In addition, the sheet element and the selectivelywater vapor transmissible barrier material laminated to at least oneside of the sheet element are formed into the desired corrugated shapeusing only one forming step (“one-step forming”). Thus, in the enthalpyexchanger element according to the invention, total (i.e. sensible pluslatent) energy transfer efficiency is increased on the one hand whilemanufacturing cost is reduced on the other hand.

Alternatively, the sequence of steps b) and c) in the method may beswitched, i.e. forming the (not yet laminated) sheet element into adesired shape exhibiting a three-dimensional corrugation pattern andthen laminating at least one side of the formed sheet element with athin polymer film with water vapor transmission characteristics(“two-step forming”).

In particular, the method for producing enthalpy exchanger elements maycomprise a cutting step after the laminating step b). Preferably, duringsteps a) and b) an air-permeable web material, typically provided byunrolling from a roller, and a thin polymer film, typically provided byfilm extrusion, are joined together in the laminating step b) by heatfusion and/or gluing, in order to prepare a continuous air-tight webcomprising a continuous air-permeable support layer laminated with acontinuous air-tight thin polymer film with water vapor transmissioncharacteristics.

The laminating step b) is followed by the cutting step.

In a first variant, the cutting step may be an additional intermediatestep between the laminating step b) and the forming step c). Preferably,the continuous laminated web is first cut into separate laminated sheetelements comprising an air-permeable support layer laminated with acontinuous air-tight thin polymer film with water vapor transmissioncharacteristics. Next, each of the laminated sheet element is formedinto a desired shape exhibiting a three-dimensional corrugation pattern.In other words, the continuous laminated web is first fed through acutting station comprising a cutting tool and then through a formingstation comprising a forming tool.

In a second variant, the cutting step may be an additional step withinthe forming step c), i.e. a part of the forming step. Preferably, thecontinuous laminated web is simultaneously cut and formed into separatelaminated sheet elements comprising an air-permeable support layerlaminated with a continuous air-tight thin polymer film with water vaportransmission characteristics and having a desired shape exhibiting athree-dimensional corrugation pattern. In other words, the continuouslaminated web is fed through a combined cutting and forming stationcomprising a cutting tool and a forming tool. Preferably, the cuttingtool and the forming tool are associated to each other, preferablycoupled to each other. They may be rigidly coupled to each other orresiliently coupled to each other. As a first alternative, the cuttingtool and the forming tool may have a positional relationship such thatduring the combined cutting and forming step the cutting tool engagesthe laminated web before the forming tool engages the laminated web. Asa second alternative, the cutting tool and the forming tool may have apositional relationship such that during the combined cutting andforming step the cutting tool engages the laminated web at the same timeas the forming tool engages the laminated web. As a third alternative,the cutting tool and the forming tool may have a positional relationshipsuch that during the combined cutting and forming step the cutting toolengages the laminated web after the forming tool engages the laminatedweb.

Water vapor transmission characteristics means a water vaportransmission rate of at least 500 g/m²/24 h, preferably of at least 1000g/m²/24 h, even more preferably of at least 1500 g/m²/24 h and mostpreferred of at least 2000 g/m²/24 h, as measured using the upright cupmethod according to modified ASTM E 96-66 B; modifications:T_(water)=30° C., T_(air)=21° C., rel. humidity=60%, air flow=2 m/s.

Step c) of forming the laminated sheet element into a desired shapeexhibiting a three-dimensional corrugation pattern may include a firststep c1) and a second step c2).

Step c1) comprises forming a first corrugation pattern or reinforcingcorrugation pattern with corrugations extending in a first direction andhaving a relatively fine structure. The first corrugation pattern mayhave a sinusoidal, rectangular or triangular periodic profile.Preferably, this first periodic profile of the first corrugation patternhas a period of 0.5 mm to 2 mm and an amplitude of 0.5 mm to 1 mm. Thefirst corrugation pattern may comprise adjacent ridges. There may be aspacing between neighboring ridges, i.e. the space of the laminated ornot yet laminated sheet element between neighboring ridges is asubstantially flat region and the neighboring ridges may protrude in thesame or in opposite directions from the sheet element. The height ordepth as well as the width of these individually located ridges may be0.2 mm to 1 mm. The ridge spacing may be 1 to 10 times the ridge width.

This optional first step c1) contributes to the overall stiffness of theenthalpy exchanger element.

Step c2) comprises forming a second corrugation pattern or maincorrugation pattern with corrugations extending in a second directionand having a relatively coarse structure defining the heat exchangerplate channel cross section geometry. Again, the second corrugationpattern may have a sinusoidal, rectangular or triangular periodicprofile, but with larger dimensions than the first corrugation pattern.Preferably, this second periodic profile of the second corrugationpattern has a period of 2 mm to 10 mm and an amplitude of 2 mm to 10 mm.

As a result, the optional first step c1) and the necessary second stepc2) provide an enthalpy exchanger element with double corrugation andenhanced rigidity.

The first direction, i.e. the direction of the ridges of the firstcorrugation pattern, forms an angle with respect to the seconddirection, i.e. the direction of the ridges of the second corrugationpattern, preferably an angle of 45° to 90°, more preferably an angle of85° to 90° and most preferably about 90°.

The sheet material of the sheet element may comprise a polymer,preferably a thermoplastic polymer. Thus, the sheet element lends itselffor instance to thermal processing in the forming step c). Preferably,polystyrene (PS), polyvinyl chloride (PVC), viscose or polyester, suchas polyethylene terephthalate (PET), or co-polyester are selected asthermoplastic polymer. Preferably, the polymer of the sheet materialdoes not include any plasticizer. The polymer of the sheet material mayinclude a biocide (bactericide and/or fungicide).

In a preferred embodiment, the sheet element is a fabric, preferably anonwoven fabric. The fabric may include thermoplastic fibers only or acombination of thermoplastic fibers and thermoset fibers or acombination of thermoplastic fibers and a resin or a combination ofthermoplastic fibers and inorganic fibers. Most preferably, the fabricincludes multicomponent or bicomponent fibers together with standardthermoset and/or thermoplastic fibers. Preferably, the fabric includesmore than 50 wt. % multicomponent or bicomponent fibers and may includemulticomponent or bicomponent fibers only. In addition, the fabric mayinclude metal fibers and/or wick fibers providing high thermalconductivity together with mechanical strength and high capillary action(“humidity conductivity”), respectively. The inorganic fibers may beglass fibers, silicon carbide fibers or any mineral fiber.

Alternatively, the sheet element is a woven fabric, preferably having ananisotropic structure and anisotropic properties resulting therefrom.For instance, the woven fabric may have thicker polymer fibers in afirst fiber direction and thinner polymer fibers in a second fiberdirection. The second fiber direction may be between 90° and 100°,preferably about 90°, with respect to the first fiber direction. Due tothe thicker polymer fibers in the first fiber direction, the anisotropicwoven fabric can withstand more stretching along the first fiberdirection without being mechanically weakened (or even damaged) thanalong the second fiber direction with thinner polymer fibers.

Alternatively, the sheet element may comprise a nonwoven fabric whichmay have an anisotropic structure and anisotropic properties resultingtherefrom, and a woven fabric, preferably having an anisotropicstructure and anisotropic properties resulting therefrom.

The sheet element may comprise additional reinforcement fibers forproviding extra strength. These reinforcement fibers may be at least oneof metal fibers, carbon fibers or thermoplastic polymer fibers. Thereinforcement fibers may extend in a first general direction within thesheet element. Preferably, the reinforcement fibers are non-straight. Inparticular, they may have a wave-like pattern, e.g. with a triangular orsinusoidal flat pattern, preferably having periods of 1 mm to 3 mm andamplitudes of 1 mm to 3 mm. Alternatively, they may have a curly shape,e.g. a helical shape, preferably having a helix diameter of less than 1mm.

The reinforcement fibers may be continuous fibers or staple fibers withminimum length of 5 mm. The metal fibers may be selected from aluminum,copper, silver or steel fibers having a diameter between 10 μm and 200μm, preferably between 20 μm to 100 μm.

Preferably, the first general direction of the wave-like pattern and/orthe curly shape of the reinforcement fibers form an angle with respectto the direction of the second corrugation pattern defining the heatexchanger plate channel cross section geometry. Preferably, they form anangle of 45° to 90°, more preferably an angle of 85° to 90° and mostpreferably an angle of about 90° with respect to each other.

During step c) or in particular during steps c1) and c2), but primarilyduring step c2), the non-straight reinforcement fibers are straightenedout. In particular, the wave-like pattern and/or the curly shape isstretched and thus flattened in profile, i.e. the amplitude of thewave-like pattern is reduced and its period is increased and/or thediameter of the curly/helical shape is reduced and its period (or pitch)is increased. Once the non-straight carbon and/or metal fibers arecompletely straightened out, the sheet element will be prevented fromfurther stretching along the first general direction.

In addition, if the sheet element is heated beyond the softeningtemperature of the thermoplastic polymer fibers before or during step c)or in particular before or during steps c1) and/or c2), thethermoplastic fibers will be deformed by undergoing local stretchingand/or bending. After the forming step c) or the forming steps c1) andc2), the permanent deformation of the thermoplastic polymer fibers willcontribute to the dimensional stability, i.e. shape retention, of theenthalpy exchanger element.

Preferably, if carbon fibers are included within the sheet element, theyextend along the second direction of the second (main) corrugationpattern. Thus, during forming step c) or during forming sub step c2),the carbon fibers will not undergo any bending. However, they contributeto the overall strength of the sheet element before and after theforming step c) or c2).

Preferably, if metal fibers are included within the sheet element, theymay extend along whatever directions within the sheet element. Thus,during forming step c) or during forming sub step c2), the metal fiberswill undergo bending under metal cold deformation conditions even if thesheet element is heated beyond the softening temperature ofthermoplastic polymer fibers. After the forming step c) or the formingsteps c1) and c2), the permanent deformation of the metal fibers willcontribute to the dimensional stability, i.e. shape retention, of theenthalpy exchanger element.

Preferably, the fibers of the fabric have fiber diameters between 1 μmand 40 μm, more preferably between 3 μm and 40 μm and most preferablybetween 5 μm and 20 μm. As a result, when the fabric is laminated withthe thin polymer film with water vapor transmission characteristics inthe laminating step b), the fabric fibers in direct contact with thethin polymer film will cover only a small portion of the surface of thethin polymer film, thus minimizing any blocking of the thin polymerfilm. In addition, even if not permanently deformed as described abovefor thermoplastic polymer fibers or metal fibers, any fabric fibersundergoing elastic bending during step c) will have a high degree offlexibility which helps make the forming step c) easier to perform.

Preferably, the fibers or fabric filaments within the sheet element andin particular those at a non-laminated surface of the sheet element, mayhave linear mass densities (filament weights) between 1 and 10 dtex (1tex=1 g/1000 m; 1 dtex=1 g/10000 m). Such fine fibers exhibit a strongwicking effect alloying them to transport humidity faster. In addition,when used at a sheet surface or at both sheet surfaces, they provide asmoother and less abrasive surface. First, this helps reduce the risk ofdamage to a very thin adjacent functional membrane layer laminated tothe respective surface. Second, this helps prevent the formation any airboundary layer at a non-laminated sheet surface.

The fibers of the fabric may have substantially circular, triangular oroval cross-sections. Also, the fibers of the fabric may have X-type orstar-like cross-sections. The fabric may include fibers having differentcross-sections, preferably chosen from the mentioned types ofcross-sections.

In addition, the fabric may include a surface impregnant, preferably athermoplastic or thermoset polymer, in order to improve structuralstability after the forming step. In addition or as an alternative, thefabric may include a surface impregnant which can be cross-linked afterthe forming step c), preferably a resin which can be cured by UVirradiation after the forming step c).

The fabric or the enthalpy exchanger element may include ahydrophobically treated layer on one of its sides and a thin polymerfilm on the other side, i.e. a single water repellant impregnation.

This can be achieved by laminating only one side of the fabric with athin polymer film with water vapor transmission characteristics in stepb) and providing the other side of the fabric with a hydrophobizationtreatment before, during or after the laminating step b). Thehydrophobization treatment may be carried out even after the formingstep c).

Preferably, the hydrophobization treatment of the fabric is carried outbefore the laminating step b). i.e. before, during or after theproviding step a). This prevents the thin polymer film with water vaportransmission characteristics to be accidentally rendered hydrophobic onits surface facing the fabric.

The fabric or the enthalpy exchanger element may include ahydrophobically treated layer on both of its sides and a thin polymerfilm inside extending in between and “in parallel” to the firsthydrophobically treated layer and to the second hydrophobically treatedlayer of the fabric or the enthalpy exchanger element, i.e. a doublewater repellant impregnation.

This can be achieved by the following steps:

First, providing one side of a first fabric or the entire first fabricwith a hydrophobization treatment before, during or after any laminatingstep b).

Second, providing one side of a second fabric or the entire secondfabric with a hydrophobization treatment before, during or after anylaminating step b).

Third, laminating one side of the first fabric with a first side of athin polymer film with water vapor transmission characteristics.

Fourth, laminating one side of the second fabric with a second side ofthe thin polymer film with water vapor transmission characteristicsproducing a sandwich structure having the thin polymer film sandwichedbetween the first fabric and the second fabric.

Finally, according to step c), this laminated sheet element having afirst fabric/thin film/second fabric type sandwich structure is formedinto a desired shape exhibiting the three-dimensional corrugationpattern.

Preferably, steps three and four are carried out at the same time, i.e.co-laminating or one-step laminating the first fabric and the secondfabric with the one thin polymer film with water vapor transmissioncharacteristics producing the sandwich structure with the thin polymerfilm sandwiched between the two fabric sheets.

Preferably, the hydrophobization treatment of the first fabric and/orthe second fabric is carried out before any laminating step b). i.e.before, during or after the fabric providing step a). Again, thisprevents any thin polymer film with water vapor transmissioncharacteristics to be accidentally rendered hydrophobic on its surfacefacing the fabric, i.e. first fabric or the second fabric.

Instead, the hydrophobization treatment of the first fabric and/or thesecond fabric may be carried out after the forming step c).

The sheet element may be composed of one layer of fabric comprising anyof the combinations of fibers mentioned in the previous paragraph.Alternatively, the sheet element may be composed of several, preferablytwo or three, stacked layers of fabric attached to each other and eachcomprising a different one of the combinations of fibers mentioned inthe previous paragraph.

The several stacked layers of fabric may have different filamentweights. They may comprise a first layer having relatively finefilaments, e.g. 1 to 10 dtex, and a second layer having relativelycoarse filaments, e.g. 10 to 40 dtex.

Preferably, the second layer with the coarser or heavier filaments isattached to the thin polymer film (membrane), providing a small directcontact area between the sheet element surface and the thin polymer filmattached to it, thus increasing the active membrane surface area of thethin polymer film. Preferably, at least a portion of the heavierfilaments are bicomponent fibers allowing the thin polymer film to beattached to the sheet element surface with less glue or no glue at all.

Alternatively, depending on the type of filaments, it can beadvantageous if the first layer with finer filaments is contacted withand attached to the thin polymer film (membrane), providing a smoothsurface at the sheet element/thin polymer film interface that does notdamage the polymer film during the forming step c) of forming thecorrugation pattern or during the forming sub step c2) of forming thesecond corrugation pattern or during end use.

Irrespective of its position within the sheet element, the second layerwith heavier or thicker filaments will provide an open and highly airand vapor permeable layer of the sheet element.

In addition, the sheet element may comprise fine filaments or fiberswith strong wicking properties to enhance transport of humidity throughthe sheet element. Preferably, the fine filaments or fibers, whenmeasured according to DIN 53924, exhibit rising heights of at least 30to 60 mm after 30 seconds and more preferably rising heights of at least40 to 60 mm after 30 seconds.

If the forming in step c) or in step c2) is done by vacuum forming withthe support of an upper pleating tool, the sheet element may have anasymmetric structure across its thickness. In particular, it may have alayer with relatively fine filaments on the vacuuming side, providinggood replication of the mold geometry, and relatively coarse filamentsfacing the upper pleating tool, providing the required structuralstrength to the sheet element.

The sheet element may comprise a layer of nonwoven fabric and a layer ofwoven fabric attached to each other. Preferably, the woven fabric has ananisotropic structure and anisotropic mechanical properties resultingtherefrom, as described above.

A portion of the fibers within the sheet element, preferably 5 to 60 wt.%, may be hollow fibers. A portion of the fibers within the sheetelement, preferably 20 to 70 wt. %, may be bicomponent fibers. Thesebicomponent fibers may have circular and/or non-circular cross sections.

A portion of the fibers within the sheet element, preferably 5 to 60 wt.%, may be hydrophilic fibers showing strong wicking properties toincrease transport of humidity. Preferably, such wicking fibers arehydrophilic on their surface and hydrophobic in their center.

A portion of the fibers within the sheet element, preferably 5 to 30 wt.%, may be water absorbing fibers, preferably hydro polymers, to create awater buffer for excess humidity.

The sheet element may have a textured surface and/or an integrated gridstructure.

As a result, this type of sheet element will cover a minimum surfacearea of the adjacent thin polymer film attached to the sheet element.The integrated grid structure may be the above-described first orreinforcing corrugation pattern formed in the first forming step c1).

In addition or as an alternative to the above-described measures forincreasing the structural strength of the sheet element,

1) hydroentanglement and/or spunlacing; and/or2) surface texturing; and/or3) integration of a grid structure with a pattern adapted to thegeometry of the second or main corrugation pattern may be applied to thenot yet laminated sheet element before subsequent lamination.

In addition or as an alternative to the above-described measures forincreasing the structural strength and the formability of the sheetelement, the sheet element may be made with an anisotropic fiberdistribution providing higher overall strength of the sheet elementand/or higher strength in a preferred direction of the sheet element. Inparticular, as mentioned above, the anisotropic fiber distribution maybe provided by at least one of carbon fibers, metal fibers orthermoplastic polymer fibers included in at least one of the severallayers of the sheet element.

Preferably, the metal fibers and/or thermoplastic polymer fibers areoriented in close-to-orthogonal relationship with respect to the seconddirection of the second (main) corrugation pattern or they may extendalong whatever directions within the sheet element. Preferably, thecarbon fibers are oriented in parallel to the second direction of thesecond (main) corrugation pattern.

The laminating step b) may comprise bonding, preferably heat bonding,welding and/or gluing, of the thin polymer film to the sheet element.Preferably, a thermoplastic adhesive (hot melt adhesive), a thermosetadhesive or a UV-curable adhesive is used for the bonding between thepolymer film and the sheet element.

In a preferred embodiment, the thin polymer film is a monolithicmembrane, i.e. a poreless membrane exhibiting a solution-diffusiontransport mechanism for individual water molecules. Preferably, thismonolithic membrane has a maximum elongation between 100% and 300%, morepreferably between 150% and 200%.

In a further preferred embodiment, the thin polymer film is a multilayerfilm comprising a sequence of polymer layers of different polymer types.Thus, with a few given polymer types, thin polymer films of differentwater vapor transmission characteristics can be designed and produced.

Preferably, the polymer type of each polymer layer is selected from thegroup consisting of polyether ester, polyether amide and polyetherurethane.

Preferably, the total thickness of the thin polymer multilayer film isbetween 5 μm and 200 μm, more preferably between 10 μm and 150 μm.

The thickness of each individual polymer layer within the thin polymermultilayer film may be between 1 μm and 20 μm, preferably between 4 μmand 20 μm and most preferably between 4 μm and 15 μm.

In general, the polymer film(s) or polymer layer(s) should be as thin aspossible for high transport rates. In the setup of the enthalpyexchanger element according to the invention, the limiting layer fortransport of water vapor is the three-dimensional sheet element locatednext to the one polymer laminate or between the two polymer laminates.In order to achieve mechanical strength and robustness of thelaminate(s) on the one hand and high transport rates on the other hand,a setup is chosen with a polymer film (laminate) thickness between 1 μmand 20 μm, preferably between 4 μm and 20 μm and most preferably between4 μm and 15 μm. Also, the three-dimensional sheet element is a thin aspossible and as permeable as possible. Preferably, the sheet element isa fabric having a thickness between 200 μm and 600 μm, preferablybetween 300 μm and 500 μm. Preferably, the sheet element is a fabrichaving a fiber volume portion between 10% and 65% of the fabric volume,preferably between 20% and 50% of the fabric volume.

Preferably, the thermoplastic polymer(s) of the thin polymer film doesnot include any plasticizer. Instead, the thin polymer film may includea biocide (bactericide and/or fungicide). The biocide will help preventgrowth of bacteria and fungi on the polymer and thus achieve longeroperation periods without cleaning.

As mentioned above with respect to the thermoplastic polymer, theforming step c) may be a pleating step or thermoforming step, preferablya vacuum forming step. At least a first mold part (e.g. lower tool)having first corrugation formations co-defining the predeterminedcorrugation pattern of the enthalpy exchanger element to bemanufactured, is provided in the thermoforming step. In addition to theat least first mold part, a second mold part (e.g. upper tool) havingsecond corrugation formations complementary to the first corrugationformations and/or a forming vacuum co-defining the predeterminedcorrugation pattern of the enthalpy exchanger element to bemanufactured, is/are provided in the thermoforming step.

Preferably, prior to the actual forming operation of the laminated sheetelement at a specific predetermined forming temperature of the firstmold part or at specific predetermined forming temperatures of the firstand second mold parts, the laminated sheet element is preheated to apreheating temperature a few degrees below the forming temperature,preferably to a preheating temperature between 5K and 30K below itsforming temperature, more preferably between 10K and 20K below itsforming temperature. For pleating, the preheating temperature of thelaminated sheet may be lower. Preferably, for pleating, the preheatingtemperature is 10K to 40 K below the forming temperature, morepreferably between 15K and 30K below the forming temperature of thelaminated sheet.

Preferably, prior to the forming step, the laminated sheet is preheatedthroughout its thickness to a uniform preheating temperature. Thisallows all the polymer fibers to be heated close to their softening ormelting temperature. Preferably, the fabric inside the laminated sheetcomprises multicomponent fibers having a first polymer material at theirsurface and a second polymer material inside the multicomponent fibersand with the first polymer material having a lower softening or meltingpoint than the second polymer material. Preferably, the multicomponentfibers are bicomponent fibers.

Preferably, at least the multicomponent fibers comprise a polymermaterial having polar functional groups. More preferably, at least thefirst polymer material at the multicomponent fibers' surface comprisespolar functional groups. Alternatively, only the first polymer materialat the multicomponent fibers' surface comprises polar functional groups.

Preferably, when multicomponent fibers are included in the laminatedsheet, the preheating temperature of the laminated sheet is atemperature between the melting point or softening point of the firstpolymer material of the multicomponent fibers at their surface and themelting point or softening point of the second polymer material insidethe multicomponent fibers.

Alternatively, when multicomponent fibers are included in the laminatedsheet, the preheating temperature of the laminated sheet is atemperature between the melting point of the first polymer material ofthe multicomponent fibers at their surface and the melting point of thesecond polymer material inside the multicomponent fibers.

Preferably, the forming temperature is provided by internally heatedfirst and/or second mold parts.

Preferably, the preheating temperature is provided by exposing the notyet formed laminated sheet to electromagnetic radiation (e.g. atinfrared or microwave frequencies) and/or to mechanical waves (e.g. atultrasonic frequencies).

The invention also provides an enthalpy exchanger element, preferablyproduced using the method as defined in the previous paragraphs,including a sheet element and a predetermined corrugation pattern,wherein a first thin polymer film is laminated to a first side of thesheet element and/or a second thin polymer film is laminated to a secondside of the sheet element, both thin polymer films having water vaportransmission characteristics.

The first thin polymer film and the second thin polymer film may beidentical to each other. If both sides of the sheet element arelaminated, an enthalpy exchanger element having excellent hygienicproperties is obtained. If only one side of the sheet element islaminated, the thermoplastic polymer of the sheet material preferablyundergoes a hydrophobization treatment and/or includes a biocide(bactericide and/or fungicide) and again, an enthalpy exchanger elementhaving excellent hygienic properties is obtained.

The first thin polymer film and the second thin polymer film may bedifferent from each other. This provides additional freedom to adjustand optimize the heat and moisture transfer characteristics of theenthalpy exchanger element.

Finally, the invention provides an enthalpy exchanger having at leastthree sheet-like or plate-like enthalpy exchanger elements as defined inany of the previous paragraphs, which are stacked onto and fixed to eachother with their respective corrugation patterns in orthogonal orparallel orientation to form orthogonal or parallel fluid paths allowingfluids to flow there through. The individual enthalpy exchanger elementsmay be fixed to each other and sealed by welding, preferably using pinchwelding or laser welding, and/or gluing, preferably using epoxy.

In order to achieve this object, the invention provides a method forproducing an enthalpy exchanger comprising the steps of

a) providing an air-permeable sheet element;b) laminating at least one side of the sheet element with a thin polymerfilm with water vapor transmission characteristics;c) forming the laminated sheet element into a desired shape exhibiting athree-dimensional corrugation pattern;d) repeating steps a), b) and c) to produce a plurality of laminated andformed sheet elements exhibiting a three-dimensional corrugationpattern;e) stacking the plurality of laminated and formed sheet elements; andf) fixing the stacked laminated and formed sheet elements to each other.

In a first variant, the laminated and formed sheet elements are stackedsuch that the corrugation patterns of adjacent elements in the stack areparallel to each other. As a result, a counter-flow enthalpy exchangeris obtained.

In a first variant, the laminated and formed sheet elements are stackedsuch that the corrugation patterns of adjacent elements in the stack areorthogonal to each other. As a result, a cross-flow enthalpy exchangeris obtained.

Preferably, the method comprises the steps of

a1) providing a first air-permeable sheet element;b1) laminating at least one side of the first sheet element with a thinpolymer film with water vapor transmission characteristics;c1) forming the first laminated sheet element into a first desired shapeexhibiting a first three-dimensional corrugation pattern;d1) repeating steps a1), b1) and c1) to produce a plurality of laminatedand formed first-type sheet elements exhibiting a firstthree-dimensional corrugation pattern;a2) providing a second air-permeable sheet element;b2) laminating at least one side of the second sheet element with a thinpolymer film with water vapor transmission characteristics;c2) forming the second laminated sheet element into a second desiredshape exhibiting a second three-dimensional corrugation pattern;d2) repeating steps a2), b2) and c2) to produce a plurality of laminatedand formed second-type sheet elements exhibiting a secondthree-dimensional corrugation pattern;e) stacking the plurality of laminated and formed first-type sheetelements and second-type sheet elements to obtain a stack withalternating first-type sheet elements and second-type sheet elements;andf) fixing the stacked laminated and formed sheet elements to each other.

Preferably, the first-type sheet elements have a first shape and thesecond-type sheet elements have a second shape complementary to thefirst shape. In particular the first-type sheet elements areright-handed sheet elements and the second-type sheet elements areleft-handed sheet elements.

In the following description, two non-limiting embodiments of theinvention are described in further detail below with reference to thedrawings, wherein:

FIG. 1 is a schematic representation of the method for producingenthalpy exchanger elements according to the invention;

FIG. 2 is a schematic representation of an enthalpy exchanger accordingto the invention or a portion thereof including a plurality of enthalpyexchanger elements according to the invention;

FIG. 3 is a SEM (scanning electron microscope) micrograph of across-sectional view of a portion of an intermediate product producedduring the method for producing an enthalpy exchanger element accordingto the invention;

FIG. 4 is a SEM micrograph of a cross-sectional view of a portion of anenthalpy exchanger element produced by the method according to theinvention;

FIG. 5 is a SEM micrograph similar to the one of FIG. 3 showing of alarger scale cross-sectional view of a smaller portion of anintermediate product produced during the method for producing anenthalpy exchanger element according to the invention;

FIG. 6 is a SEM micrograph similar to the one of FIG. 4 showing of asmaller scale cross-sectional view of a larger portion of an enthalpyexchanger element produced by the method according to the invention;

FIG. 7 is a schematic perspective view showing a right-handed enthalpyexchanger sheet element of a first embodiment according to theinvention;

FIG. 8 is a schematic plan view showing the right-handed enthalpyexchanger sheet element of the first embodiment according to theinvention;

FIG. 9 is a schematic perspective view showing a left-handed enthalpyexchanger sheet element of a second embodiment according to theinvention;

FIG. 10 is a schematic plan view showing the left-handed enthalpyexchanger sheet element of the second embodiment according to theinvention;

FIG. 11 is a schematic perspective view showing a right-handed enthalpyexchanger sheet element of the second embodiment according to theinvention;

FIG. 12 is a schematic plan view showing the right-handed enthalpyexchanger sheet element of the second embodiment according to theinvention; and

FIG. 13 is a schematic plan view showing a pair of enthalpy exchangersheet elements stacked one on top of the other, one being theleft-handed enthalpy exchanger sheet element as shown in FIG. 10 and theone other being the right-handed enthalpy exchanger sheet element asshown in FIG. 12.

In FIG. 1, a schematic representation of the method for producingenthalpy exchanger elements according to the invention is shown.Cross-sections of the intermediate products, i.e. the results of each ofsteps S1, S2 and S3, are shown.

In a first step S1, an air-permeable sheet element 1 having voids oropenings 2 is provided.

In a second step S2, both sides 1 a, 1 b of the sheet element 1 arelaminated with a thin polymer film 3, 4 with water vapor transmissioncharacteristics.

In a third step S3, the laminated sheet element 1 is formed into adesired shape exhibiting a three-dimensional corrugation pattern 5.

The sheet element 2 is a non-woven fabric including thermoplastic fibersonly or a combination of thermoset fibers and thermoplastic fibers. Thefabric may include bicomponent fibers together with standard thermosetand/or thermoplastic fibers.

The thin polymer film 3, 4 is a multilayer film which may comprise asequence (not shown) of polymer layers of different polymer types.

The forming step S3 is a thermoforming step, preferably a vacuum formingstep. At least a first mold part (e.g. lower tool, not shown) havingfirst corrugation formations co-defining the predetermined corrugationpattern 5 of the enthalpy exchanger element E, E′ to be manufactured, isused in the thermoforming step S3. In addition to the at least firstmold part, a second mold part (e.g. upper tool, not shown) having secondcorrugation formations complementary to the first corrugation formationsand/or a forming vacuum co-defining the predetermined corrugationpattern of the enthalpy exchanger element E, E′ to be manufactured,is/are used in the thermoforming step S3.

The resulting enthalpy exchanger element E having a first thin polymerfilm 3 on the first side 1 a of the sheet element 1 and a second thinpolymer film 4 on the second side 1 b of the sheet element 1 comprises acorrugated structure 5 with alternating squeezed portions 5 a andsqueezed/stretched portions 5 b. The squeezed portion 5 a extend in afirst direction (horizontal direction in FIG. 1) and thesqueezed/stretched portions 5 b extend in a second direction differentfrom the first direction. Preferably, the angle α between the firstdirection and the second direction in the corrugation pattern 5 of theenthalpy exchanger element E is between 90° and 120°, preferably between95° and 105°, an example of which is shown in FIG. 1. Alternatively,unlike the example shown in FIG. 1, the angle α between the firstdirection and the second direction in the corrugation pattern 5 of theenthalpy exchanger element E is between 80° and 90°, preferably between85° and 90°.

In FIG. 2, a schematic representation of a first type enthalpy exchangerE1-E2-E3 or second type enthalpy exchanger E1 ‘-E2’-E3′ according to theinvention is shown. The first type E1-E2-E3 includes a plurality ofenthalpy exchanger elements E1, E2, E3 where the first thin polymer film3 and the second thin polymer film 4 (FIG. 1) are films of the sametype. The second type E1 ‘-E2’-E3′ includes a plurality of enthalpyexchanger elements E1′, E2′, E3′ where the first thin polymer film 3 andthe second thin polymer film 4 (FIG. 1) are films of different typesincluding the case where one of the two films 3, 4 has zero thickness,i.e. the enthalpy exchanger element has only one thin polymer film 3 or4 on one side 1 a or 1 b of the sheet element 1.

In FIG. 2, the outer walls of the housing/packaging of the enthalpyexchanger E1-E2-E3 or E1 ‘-E2’-E3′ is not shown. The air inlet/outletportions (not shown) of the enthalpy exchanger E1-E2-E3 or E1 ‘-E2’-E3′are provided with air distribution patterns such that the air flowdirection in adjacent air ducts in the enthalpy exchanger E1-E2-E3 or E1‘-E2’-E3′ are in opposite directions, as shown by the 0 symbolindicating air flow towards the viewer and the X symbol indicating airflow away from the viewer.

FIG. 3 shows a SEM (scanning electron microscope) micrograph of across-sectional view of an air-permeable sheet element 1 laminated onits upper side 1 a with a first thin polymer film 3 and laminated on itslower side 1 b with a second thin polymer film 4 as a result of step b)of the method according to the invention.

The laminating step b) may comprise bonding, preferably heat bondingand/or gluing, of the thin polymer films 3, 4 to the sheet element 1. Athermoplastic adhesive (hot melt adhesive) may be used for the bondingbetween the polymer film 3 and 4 and the sheet element 1.

The sheet element 1 is a nonwoven fabric comprising a plurality offibers 6. The fibers 6 may be thermoplastic fibers only or a combinationof thermoset fibers and/or mineral fibers on the one hand andthermoplastic fibers on the other hand. Most preferably, the fabricincludes multicomponent or bicomponent fibers together with standardthermoset and/or thermoplastic fibers. As can be best seen by comparingFIG. 3 with FIG. 4, the fibers 6 of the nonwoven fabric sheet element 1shown in FIG. 3 are less densely packed than the fibers 6 of thenonwoven fabric sheet element 1 of the enthalpy exchanger element shownin FIG. 4.

FIG. 4 shows a SEM micrograph of a cross-sectional view of a portion ofan enthalpy exchanger element E produced by forming the laminated sheetelement 1 of FIG. 3 into a desired shape exhibiting a three-dimensionalcorrugation pattern as a result of step c) of the method according tothe invention.

The forming step c) may be a pleating step or thermoforming step,preferably a vacuum forming step. At least a first mold part (e.g. lowertool, not shown) having first corrugation formations defining orco-defining the predetermined corrugation pattern of the enthalpyexchanger element E, E′ to be manufactured, is provided for and used inthe thermoforming step. In addition to the at least first mold part, asecond mold part (e.g. upper tool, not shown) having second corrugationformations complementary to the first corrugation formations and/or aforming vacuum co-defining the predetermined corrugation pattern of theenthalpy exchanger element E, E′ to be manufactured, may be provided inthe thermoforming step.

The first mold part (e.g. lower tool) may comprise nozzles or throughholes pneumatically connected to a vacuum source providing a vacuum forthe vacuum forming step.

In addition to the first mold part and/or the second mold part used inthe forming step c), preferably for supporting the vacuum action in thevacuum forming step, nozzles connected to a pressurized air source maybe provided. These nozzles may be provided in the vicinity of,preferably adjacent to, the first mold part and/or the second mold part.Preferably, the pressurized air source comprises an air heating devicefor heating the pressurized air.

The combined use of the first tool and the vacuum source in thethermoforming step c) can be supplemented by the second tool and/or thepressurized air source, preferably with an air heating device. As aresult, using at least some of these supplements, a sheet element 1laminated with a first thin polymer film 3 and an optional second thinpolymer film 4 can be pressed more strongly against the firstcorrugation formations of the first mold part, thus producing anenthalpy exchanger element E with a better copy of the first corrugationformations of the first mold part defining or co-defining thepredetermined corrugation pattern of the enthalpy exchanger element E tobe manufactured.

The sheet element 1 of the enthalpy exchanger element E has its fibers 6much more densely packed than the sheet element 1 of FIG. 3. During thepleating or thermoforming step c), the fabric sheet element 1 with itsfirst thin polymer film 3 and its second thin polymer film 4 iscompressed and heated. At least the thermoplastic fibers or themulticomponent or bicomponent fibers of the plurality of fibers 6 aresoftened or partly melted during the pleating or thermoforming step c).

As a result, after cooling and hardening of the thermoplastic fibers orthe multicomponent or bicomponent fibers of the plurality of fibers 6,the fabric sheet element 1 with its first thin polymer film 3 and itssecond thin polymer film 4 is transformed into an enthalpy exchangerelement E according to the invention with a more compact fiber structurein the fabric sheet element 1 and with a three-dimensional corrugationpattern.

FIG. 5 shows a SEM micrograph similar to the one of FIG. 3 showing of alarger scale cross-sectional view of a smaller portion of theair-permeable fabric sheet element 1 laminated on its upper side 1 awith the first thin polymer film 3 and laminated on its lower side 1 bwith the second thin polymer film 4 as a result of step b) of the methodaccording to the invention.

FIG. 6 shows a SEM micrograph similar to the one of FIG. 4 showing of asmaller scale cross-sectional view of a larger portion of the enthalpyexchanger element E produced by the method according to the invention.

FIG. 7 and FIG. 8 are a schematic perspective view and a schematic planview, respectively of a right-handed enthalpy exchanger sheet element PRof a first embodiment according to the invention. The plate-likeenthalpy exchanger element PR has a parallel flow/counter-flow region PFcomprising the corrugation 5, a first cross-flow region CF1 upstream ofthe parallel flow/counter-flow region PF, and a second cross-flow regionCF2 downstream of the parallel flow/counter-flow region PF. A pluralityof such right-handed enthalpy exchanger sheet elements PR are stackedwith a plurality of left-handed enthalpy exchanger sheet elements PL(not shown) to form an enthalpy exchanger stack with alternatingright-handed enthalpy exchanger sheet elements PR and left-handedenthalpy exchanger sheet elements PL.

In plan view, the first and second cross-flow regions CF1 and CF2 aredelimited by a triangular contour line, i.e. they have a triangularshape. Each cross-flow region CF1 and CF2 comprises a plurality of airguiding walls 15 and 16, respectively. The air guiding walls 15 aresubstantially parallel to each other and substantially parallel to oneside of the triangular shape of the first cross-flow region CF1.Similarly, the air guiding walls 16 are substantially parallel to eachother and parallel to one side of the triangular shape of the secondcross-flow region CF2. The air guiding walls 15 of the first cross-flowregion CF1 and the air guiding walls 16 of the second cross-flow regionCF2 both extend in a direction forming an angle β of about 45° with thedirection of the corrugations 5 of the parallel flow/counter-flow regionPF. As a result, in the enthalpy exchanger stack with alternatingright-handed enthalpy exchanger sheet elements PR and left-handedenthalpy exchanger sheet elements PL, the air guiding walls 15 ofadjacent right-handed and left-handed sheet elements PR and PL extend indirections forming an angle of about 90° with respect to each other,thus defining the first cross-flow region CF1 of the enthalpy exchangerstack. Similarly, in the enthalpy exchanger stack with alternatingright-handed enthalpy exchanger sheet elements PR and left-handedenthalpy exchanger sheet elements PL, the air guiding walls 16 ofadjacent right-handed and left-handed sheet elements PR and PL extend indirections forming an angle of about 90° with respect to each other,thus defining the second cross-flow region CF2 of the enthalpy exchangerstack.

A first transition region 18 extends between the first cross-flow regionCF1 and the parallel flow/counter-flow region PF. A second transitionregion 19 extends between the second cross-flow region CF2 and theparallel flow/counter-flow region PF. Both transition regions 18 and 19comprise open ends and closed ends of the corrugations 5 and theparallel air ducts formed by the corrugations such that eachclosed-ended duct has an adjacent open-ended duct. The end wall of eachclosed-ended duct is sloped such that the wall forms an angle of 5° to60° with respect to the longitudinal direction of the parallel airducts. As a result, in the enthalpy exchanger stack with alternatingright-handed enthalpy exchanger sheet elements PR and left-handedenthalpy exchanger sheet elements PL, resistance to air flow isminimized in the first transition regions 18 of the enthalpy exchangerstack and in the second transition regions 19 of the enthalpy exchangerstack.

The plate-like enthalpy exchanger element PR has a plurality of stepsalong its outer contour line. In the example shown in FIGS. 7 and 8, theplate-like enthalpy exchanger element PR has a first step 11 located atthe corner of the first triangular cross-flow region CF1, a second step12 located about halfway along the parallel flow/counter-flow region PFon one side thereof, a third step 13 located at the corner of the secondtriangular cross-flow region CF2 and a forth step 14 located abouthalfway along the parallel flow/counter-flow region PF on the other sidethereof. As a result, in the enthalpy exchanger stack with alternatingright-handed enthalpy exchanger sheet elements PR and left-handedenthalpy exchanger sheet elements PL, adjacent enthalpy exchanger sheetelements can be correctly positioned by fitting the steps 11, 12, 13, 14of a right-handed enthalpy exchanger sheet element PR with thecorresponding complementary steps 11, 12, 13, 14 of an adjacentleft-handed enthalpy exchanger sheet element PL. In other words, aright-handed sheet element PR goes “hand in hand” and fits snugly withan adjacent left-handed sheet element PL before permanently fixing thestacked sheet elements to each other.

Also, the plate-like enthalpy exchanger element PR has an offset 17located about halfway along the length of each duct formed by thecorrugations 5. As a result, in the enthalpy exchanger stack withalternating right-handed enthalpy exchanger sheet elements PR andleft-handed enthalpy exchanger sheet elements PL, adjacent enthalpyexchanger sheet elements can be correctly positioned and are preventedfrom slipping into each other during the stacking operation.

FIG. 9 and FIG. 10 are a schematic perspective view and a schematic planview, respectively of a left-handed enthalpy exchanger sheet element PLof a second embodiment according to the invention. The plate-likeenthalpy exchanger element PL has a parallel flow/counter-flow regionPF′ comprising the corrugation 5, a first cross-flow region CF1′downstream of the parallel flow/counter-flow region PF′, and a secondcross-flow region CF2′ upstream of the parallel flow/counter-flow regionPF′.

FIG. 11 and FIG. 12 are a schematic perspective view and a schematicplan view, respectively of a right-handed enthalpy exchanger sheetelement PR of the second embodiment according to the invention. Theplate-like enthalpy exchanger element PR has a parallelflow/counter-flow region PF comprising the corrugation 5, a firstcross-flow region CF1 upstream of the parallel flow/counter-flow regionPF, and a second cross-flow region CF2 downstream of the parallelflow/counter-flow region PF.

The difference between the second embodiment and the first embodiment isthe type and number of offsets. Other than that, the right-handedplate-like enthalpy exchanger elements PR and left-handed plate-likeenthalpy exchanger elements PL of the first and second embodiments areidentical. In the drawings of the first and second embodiments, the samereference numerals are used for identical features in both embodiments.

Unlike the first embodiment where the right-handed plate-like enthalpyexchanger elements PR (FIGS. 7 and 8) and left-handed plate-likeenthalpy exchanger elements PL (not shown) each have one offset 17located about halfway along the length of each duct formed by thecorrugations 5 in the plate elements PR and PL, the right-handedplate-like enthalpy exchanger elements PR (FIGS. 11 and 12) andleft-handed plate-like enthalpy exchanger elements PL (FIGS. 9 and 10)of the second embodiment each have a first offset 171 and a secondoffset 172 spaced with respect to each other along the length of eachduct formed by the corrugations 5 in the plate elements PR and PF.Again, as a result, in the enthalpy exchanger stack with alternatingright-handed enthalpy exchanger sheet elements PR and left-handedenthalpy exchanger sheet elements PL, adjacent enthalpy exchanger sheetelements PR and PL can be correctly positioned and are prevented fromslipping into each other during the stacking operation when mechanicalforce is exerted on the sheets and/or in operation when pressuredifferences between opposite air flows in adjacent parallel flow/counterflow regions PF and PF′ in the enthalpy exchanger stack or block maybuild up.

The first offset 171 and the second offset 172 each are formed as acurved longitudinal section or as an arcuate longitudinal section withinthe longitudinally extending corrugations 5 in the plate elements PR andPF. As shown in FIGS. 9, 10, 11, 12 and 13, the first offsets 171 of theright-handed plate elements PR extend in a first lateral direction withrespect to the longitudinal direction of the corrugations 5, and thefirst offsets 171 of the left-handed plate elements PL extend in asecond lateral direction opposite to the first lateral direction withrespect to the longitudinal direction of the corrugations 5. Similarly,the second offsets 172 of the right-handed plate elements PR extend inthe second lateral direction opposite to the first lateral directionwith respect to the longitudinal direction of the corrugations 5, andthe second offsets 172 of the left-handed plate elements PL extend inthe first lateral direction with respect to the longitudinal directionof the corrugations 5.

Again, a plurality of such right-handed enthalpy exchanger sheetelements PR (as shown in FIGS. 11 and 12) are stacked with a pluralityof such left-handed enthalpy exchanger sheet elements PL (as shown inFIGS. 9 and 10) to form an enthalpy exchanger stack with alternatingright-handed enthalpy exchanger sheet elements PR and left-handedenthalpy exchanger sheet elements PL. In such a stack, oppositelylaterally extending first offsets 171 of adjacent sheet elements PR andPL are positioned on top of each other. Similarly, oppositely laterallyextending second offsets 172 of adjacent sheet elements PR and PL arepositioned on top of each other. As a result, all adjacent first offsets171 and all adjacent second offsets 172 in the stack prevent thecorrugations 5 of adjacent stacks from slipping into each other duringthe stacking operation and/or in operation when pressure differencesbetween opposite air flows may build up.

FIG. 13 is a schematic plan view showing a pair of enthalpy exchangersheet elements stacked one on top of the other, the one shown withcontinuous lines being the left-handed enthalpy exchanger sheet elementPL as shown in FIG. 10 and the one shown with discontinuous lines beingthe right-handed enthalpy exchanger sheet element PR as shown in FIG.12. Such pairs of left-handed enthalpy exchanger sheet elements PL andright-handed enthalpy exchanger sheet elements PR are stacked on top ofeach other to form a complete enthalpy exchanger stack or block.

REFERENCE NUMERALS

-   1 fabric sheet element-   1 a first surface-   1 b second surface-   2 voids or openings-   3 first thin polymer film-   4 second thin polymer film-   5 corrugation(s)-   5 a squeezed portion-   5 b squeezed and/or stretched portion-   S1 providing step-   S2 laminating step-   S3 forming step (co-forming)-   O air flow direction towards viewer-   X air flow direction away from viewer-   6 fiber-   α angle (in corrugation pattern)-   PR plate-like enthalpy exchanger element, right-handed-   PL plate-like enthalpy exchanger element, left-handed-   11 step-   12 step-   13 step-   14 step-   CF1 first cross flow region of PR-   CF2 second cross flow region of PR-   PF parallel flow/counter flow region of PR-   CF1′ first cross flow region of PL-   CF2′ second cross flow region of PL-   PF′ parallel flow/counter flow region of PL-   15 air guiding walls (in CF1)-   16 air guiding walls (in CF2)-   17 offset-   171 first offset-   172 second offset-   18 first transition region (at CF1 side)-   19 second transition region (at CF2 side)-   β angle between directions of corrugations and air guiding walls

1. A method for producing enthalpy exchanger elements (E, E′, PF, PL)comprising the steps of: a) providing an air-permeable sheet element(1); b) laminating at least one side (1 a, 1 b) of the sheet element (1)with a thin polymer film (3, 4) with water vapor transmissioncharacteristics; c) forming the laminated sheet element (1) into adesired shape exhibiting a three-dimensional corrugation pattern (5, 5,. . . ).
 2. The method according to claim 1, wherein the sheet materialof the sheet element (1) comprises a polymer.
 3. The method according toclaim 1, wherein the sheet element (1) is a fabric, preferably anonwoven fabric.
 4. The method according to claim 3, wherein a fraction,preferably at least 50% by weight, of the fibers (6) of the fabric aremulti-component, preferably bi-component fibers.
 5. The method accordingto claim 1, to wherein the laminating step b) comprises at least one ofbonding, preferably heat bonding, welding and gluing, of the thinpolymer film (3, 4) to the sheet element (1).
 6. The method according toclaim 1, wherein the at least one thin polymer film (3, 4) on the atleast one side (1 a, 1 b) of the sheet element (1) is an air-impermeablepolymer film.
 7. The method according to claim 1, wherein the thinpolymer film (3, 4) is a multilayer film comprising a sequence ofpolymer layers of different polymer types.
 8. The method according toclaim 7, wherein the polymer type of each polymer layer is selected fromthe group consisting of polyether ester, polyether amide and polyetherurethane.
 9. The method according to claim 7, wherein the totalthickness of the thin polymer multilayer film is between 5 μm and 200μm, more preferably between 10 μm and 150 μm.
 10. The method accordingto claim 7, wherein the thickness of each individual polymer layerwithin the thin polymer multilayer film is between 1 μm and 20 μm,preferably between 4 μm and 20 μm, and more preferably between 4 μm and15 μm.
 11. The method according to claim 1, wherein the forming step c)is a thermoforming step, preferably a vacuum forming step or a pleatingstep.
 12. The method according to claim 11, wherein at least a firstmold part having first corrugation formations defining or co-definingthe predetermined corrugation pattern of the enthalpy exchanger element(E, E′) to be manufactured, is provided for and used in thethermoforming step c).
 13. The method according to claim 12, wherein asecond mold part having second corrugation formations complementary tothe first corrugation formations co-defining the predeterminedcorrugation pattern of the enthalpy exchanger element (E, E′) to bemanufactured, is provided for and used in the thermoforming step c). 14.The method according to claim 10, wherein nozzles connected to apressurized air source provided for and used in the thermoforming stepc).
 15. The method according to claim 14, wherein the nozzles areprovided in the vicinity of the first mold part and/or the second moldpart. 16.-24. (canceled)
 25. The method of claim 1 further comprising:d) repeating steps a), b) and c) to produce a plurality of laminated andformed sheet elements exhibiting a three-dimensional corrugationpattern; e) stacking the plurality of laminated and formed sheetelements; and f) fixing the stacked laminated and formed sheet elementsto each other.
 26. (canceled)
 27. An enthalpy exchanger element (E; E′,PR, PF), produced using the method as defined in claim 1, including anair-permeable sheet element (1) and a predetermined three-dimensionalcorrugation pattern (5, 5, . . . ), wherein a first thin polymer film(3) is laminated to a first side (1 a) of the sheet element (1) and/or asecond thin polymer film (4) is laminated to a second side (1 b) of thesheet element (1), the one or both thin polymer films (3, 4) havingcharacteristics for selective water vapor transmission.
 28. The enthalpyexchanger element (E, PR, PF) according to claim 27, wherein the firstthin polymer film (3) and the second thin polymer film (4) are identicalto each other.
 29. The enthalpy exchanger element (E′, PR, PF) accordingto claim 27, wherein the first thin polymer film (3) and the second thinpolymer film (4) are different from each other. 30.-32. (canceled) 33.An enthalpy exchanger having at least three sheet-like or plate-likeenthalpy exchanger elements (E1, E2, E3; E1′, E2′, E3′) as defined inclaim 27, which are stacked onto and fixed to each other, preferably bymeans of welding such as pinch welding, laser welding or ultrasonicwelding or by means of gluing, with their respective three-dimensionalcorrugation patterns (5, 5, . . . ) in orthogonal or parallelorientation to form orthogonal or parallel fluid paths allowing fluidsto flow there through.